Active Control of Solid Propellant Generators Using Throat Modulation Techniques and Programmable Compensation.
Abstract
A system for controlling solid propellant gas generators including a microprocessor which has inputs such as the sensed tempertures of the gases in the solid propellant gas generator, the pressure within the solid propellant gas generator and/or pre-programmed nput control signals to the microprocessor for causing the microprocessor to produce signals that are used to control a modulation valve which in turn controls a thrust nozzle device that controls exhaust gases from the solid propellant gas generator. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1982
- Accession Number
- ADD009597
Entities
People
- J. C. Dunaway
- Paul L. Jacobs
Organizations
- United States Army